17KS12000 MOTOR GRAIN STRUCTURAL INTEGRITY ANALYSIS

PDF

Authors
  1. Carrier, C.
Corporate Authors
Defence Research Establishment Valcartier, Valcartier QUE (CAN)
Abstract
As part of a Provision of Services Agreement between Bristol Aerospace Ltd. and the Department of National Defence, the Defence Research Establishment Valcartier, was required to perform the structural integrity analysis of the grain of a solid propellant rocket motor, designated as the 17KS12000. Three load cases were considered for the final analysis: thermal contraction, launch acceleration, and ignition pressurization. The analyst used the finite element method and applied the Williams-Landel-Ferry technique of reduced variables to the propellant mechanical properties.
Report Number
DREV-4196/81 —
Date of publication
15 Mar 1981
Number of Pages
71
DSTKIM No
81-02136
CANDIS No
33088
Format(s):
Document Image stored on Optical Disk;Originator's fiche received by DSIS

Permanent link

Document 1 of 1

Date modified: